Thrust Profile (N)
2.70s Burn WindowEngineered by AeroTech, the J250W is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 704.0 Ns over a 2.70 second burn window.
With an average thrust of 260.0 N and a peak of 338.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the White Lightning propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Tripoli Rocketry Association, Inc.Mass Budget
708g TotalDesign wings in your spreadsheet
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